WO2017216689A1 - Conduit et procédé pour diriger un écoulement d'air en provenance d'un dispositif refroidi par air à bord d'un avion - Google Patents

Conduit et procédé pour diriger un écoulement d'air en provenance d'un dispositif refroidi par air à bord d'un avion Download PDF

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Publication number
WO2017216689A1
WO2017216689A1 PCT/IB2017/053393 IB2017053393W WO2017216689A1 WO 2017216689 A1 WO2017216689 A1 WO 2017216689A1 IB 2017053393 W IB2017053393 W IB 2017053393W WO 2017216689 A1 WO2017216689 A1 WO 2017216689A1
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
air
duct
orifice
inlet
Prior art date
Application number
PCT/IB2017/053393
Other languages
English (en)
Inventor
Hongzhi Wang
Original Assignee
Bombardier Inc.
Short Brothers Plc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bombardier Inc., Short Brothers Plc filed Critical Bombardier Inc.
Priority to US16/309,253 priority Critical patent/US20190256213A1/en
Priority to CN201780036478.1A priority patent/CN109641662A/zh
Priority to EP17732236.9A priority patent/EP3468872B1/fr
Priority to CA3027484A priority patent/CA3027484A1/fr
Publication of WO2017216689A1 publication Critical patent/WO2017216689A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0614—Environmental Control Systems with subsystems for cooling avionics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0625—Environmental Control Systems comprising means for distribution effusion of conditioned air in the cabin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/064—Environmental Control Systems comprising more than one system, e.g. dual systems
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Definitions

  • the duct may have a curved center line and the orifice may be disposed on a concave side of the duct.
  • Duct 40 may be configured to direct the flow of exhaust air 37 away from electric motor 32 and discharge the flow of exhaust air 37 to one or both of the exterior of aircraft 10 and the interior of equipment bay 12 depending on an operating condition of aircraft 10.
  • duct 40 may comprise exhaust outlet 44 configured to discharge some of the exhaust air 37 received at inlet 42 to an exterior of aircraft 10 by discharging some of the exhaust air 37 through skin 18A of fuselage 18.
  • the portion of exhaust air 37 discharged to the exterior of aircraft 10 is labelled using reference numeral 37A in FIG. 2.
  • Duct 40 may also comprise orifice 46 disposed upstream of exhaust outlet 44 and configured to discharge some of the exhaust air 37 received at inlet 42 to an interior of equipment bay 12 (i.e. an interior of aircraft 10).
  • the portion of exhaust air 37 discharged to the interior of aircraft 10 is labelled using reference numeral 37B in FIG. 2.
  • Orifice 46 may reduce an overall downstream flow resistance to fan 38 and thereby increase the amount of air flow produced by fan 38 during one or more operating conditions of aircraft 10.
  • 10 may comprise an airspeed of aircraft 10.

Landscapes

  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Ventilation (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

L'invention concerne des conduits et des procédés destinés à diriger un écoulement d'air en provenance de dispositifs refroidis par air à bord d'avions. Un procédé décrit à titre d'exemple comporte les étapes consistant à: recevoir de l'air transportant de la chaleur extraite du dispositif, diriger l'air à l'écart du dispositif, et libérer l'air vers au moins un lieu parmi l'extérieur de l'avion et l'intérieur de l'avion. Une proportion de l'air libéré vers l'extérieur de l'avion et vers l'intérieur de l'avion est modifiée de façon passive en fonction d'une condition d'exploitation telle que la vitesse anémométrique de l'avion.
PCT/IB2017/053393 2016-06-14 2017-06-08 Conduit et procédé pour diriger un écoulement d'air en provenance d'un dispositif refroidi par air à bord d'un avion WO2017216689A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US16/309,253 US20190256213A1 (en) 2016-06-14 2017-06-08 Duct and method for directing a flow of air from an air-cooled device onboard an aircraft
CN201780036478.1A CN109641662A (zh) 2016-06-14 2017-06-08 用于对来自飞行器机载的风冷装置的空气流进行引导的管道和方法
EP17732236.9A EP3468872B1 (fr) 2016-06-14 2017-06-08 Conduit et procédé pour diriger un écoulement d'air en provenance d'un dispositif refroidi par air à bord d'un avion
CA3027484A CA3027484A1 (fr) 2016-06-14 2017-06-08 Conduit et procede pour diriger un ecoulement d'air en provenance d'un dispositif refroidi par air a bord d'un avion

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201662349706P 2016-06-14 2016-06-14
US62/349,706 2016-06-14

Publications (1)

Publication Number Publication Date
WO2017216689A1 true WO2017216689A1 (fr) 2017-12-21

Family

ID=59101533

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2017/053393 WO2017216689A1 (fr) 2016-06-14 2017-06-08 Conduit et procédé pour diriger un écoulement d'air en provenance d'un dispositif refroidi par air à bord d'un avion

Country Status (5)

Country Link
US (1) US20190256213A1 (fr)
EP (1) EP3468872B1 (fr)
CN (1) CN109641662A (fr)
CA (1) CA3027484A1 (fr)
WO (1) WO2017216689A1 (fr)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10119433C1 (de) * 2001-04-20 2002-08-22 Liebherr Aerospace Gmbh Stauluftkanal für eine Flugzeugklimaanlage
US20040160092A1 (en) * 2003-02-13 2004-08-19 Boeing Management Company Ventilated seating system with improved low pressure performance
US20060180388A1 (en) * 2005-02-14 2006-08-17 Honeywell International, Inc. Eccentric exhaust muffler for use with auxiliary power units
WO2011018381A2 (fr) * 2009-08-11 2011-02-17 Airbus Operations Limited Déflecteur des gaz d'échappement

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7153124B2 (en) * 2002-08-09 2006-12-26 The Boeing Company Preforming thermoplastic ducts
DE102008009274B4 (de) * 2008-02-15 2011-06-01 Airbus Operations Gmbh System und Verfahren zur Belüftung eines Bereichs, insbesondere eines explosionsgefährdeten Bereichs eines Luftfahrzeugs
DE102009037380B4 (de) * 2009-08-13 2013-05-29 B/E Aerospace Systems Gmbh Sauerstoffnotversorgungsvorrichtung
FR2956379B1 (fr) * 2010-02-17 2012-08-24 Technofan Appareil de ventilation pour aeronef
US9302776B2 (en) * 2012-08-15 2016-04-05 Hamilton Sundstrand Corporation Ram outlet header
US9347455B2 (en) * 2012-12-21 2016-05-24 Hamilton Sundstrand Corporation Ejector assembly

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10119433C1 (de) * 2001-04-20 2002-08-22 Liebherr Aerospace Gmbh Stauluftkanal für eine Flugzeugklimaanlage
US20040160092A1 (en) * 2003-02-13 2004-08-19 Boeing Management Company Ventilated seating system with improved low pressure performance
US20060180388A1 (en) * 2005-02-14 2006-08-17 Honeywell International, Inc. Eccentric exhaust muffler for use with auxiliary power units
WO2011018381A2 (fr) * 2009-08-11 2011-02-17 Airbus Operations Limited Déflecteur des gaz d'échappement

Also Published As

Publication number Publication date
EP3468872A1 (fr) 2019-04-17
US20190256213A1 (en) 2019-08-22
CN109641662A (zh) 2019-04-16
EP3468872B1 (fr) 2022-04-06
CA3027484A1 (fr) 2017-12-21

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